首页> 外国专利> Rotary circular aerofoil flying unit has a single rotary circular aerofoil with air channeling ribs for guiding compressed air to a nozzle outlet on the underside of the aerofoil wing section, with a radial airflow being generated

Rotary circular aerofoil flying unit has a single rotary circular aerofoil with air channeling ribs for guiding compressed air to a nozzle outlet on the underside of the aerofoil wing section, with a radial airflow being generated

机译:旋转式圆形翼型飞行器具有单个旋转式圆形翼型,带有空气引导肋,用于将压缩空气引导至翼型机翼部分下侧的喷嘴出口,并产生径向气流

摘要

Flying device comprises a rotary circular aerofoil that has air channeling ribs (2) and an aircraft wing cross-section (1Q). The circular aerofoil with its air channeling ribs forms a gyroscopic compressor. The generated air flow (3) is supplied radially to the aerofoil over the whole 360[deg] surface. The generated radial air flow does not cause rotor surface loading as with helicopters. Thus a number of circular aerofoils can be arranged on top of each other to generate a very large lift force.
机译:飞行装置包括具有空气导流肋(2)和飞机机翼横截面(1Q)的旋转圆形翼型。带有空气导流肋的圆形翼型形成了陀螺压缩机。所产生的气流(3)在整个360°表面上被径向地提供给翼型。产生的径向气流不会像直升机那样引起旋翼表面负荷。因此,可以将多个圆形翼型彼此叠置以产生很大的升力。

著录项

  • 公开/公告号DE102005059679A1

    专利类型

  • 公开/公告日2006-11-09

    原文格式PDF

  • 申请/专利权人 IWANEK GUENTER;

    申请/专利号DE20051059679

  • 发明设计人 IWANEK GUENTER;

    申请日2005-12-14

  • 分类号B64C27/22;

  • 国家 DE

  • 入库时间 2022-08-21 21:20:09

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